Calculated Wind-tunnel-boundary Lift-interference Factors for Rectangular Perforated Test Sections PDF Download
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Author: Benferd L. Schilling
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 66
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Book Description
Author: Benferd L. Schilling
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 66
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 784
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 946
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1250
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
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Book Description
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 472
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Book Description
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 470
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Book Description
Author: James D. Keller
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 26
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Book Description
A numerical method is presented for calculating the boundary-induced interference at subsonic speeds in wind tunnels of rectangular cross section with slotted or perforated walls. The slot width or wall porosity can vary throughout the test section. The interference can be computed at any point in the test section. The model can be any configuration and can be located anywhere in the test section. Several examples are given, and comparison is made with other methods were available.
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1504
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 312
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Book Description
